|Publication number||US7595612 B2|
|Application number||US 11/751,492|
|Publication date||Sep 29, 2009|
|Filing date||May 21, 2007|
|Priority date||May 21, 2007|
|Also published as||EP1995868A2, US20080290843|
|Publication number||11751492, 751492, US 7595612 B2, US 7595612B2, US-B2-7595612, US7595612 B2, US7595612B2|
|Inventors||Evgeni Ganev, Andrew R. Druzsba, Addy Fouad Alkhatib|
|Original Assignee||Honeywell International Inc.|
|Export Citation||BiBTeX, EndNote, RefMan|
|Patent Citations (17), Referenced by (3), Classifications (8), Legal Events (2)|
|External Links: USPTO, USPTO Assignment, Espacenet|
The present invention generally relates to high speed generators and, more specifically, to apparatus and methods for regulating voltage to a DC power distribution bus over a wide speed range in a high reactance permanent magnet machine based electrical power generation system.
Electrical power generation systems (PGS) play a significant role in the modern aerospace/military industry. Recently, this is particularly true in the area of more electric architecture (MEA) for aircraft and spacecraft. The commercial aircraft business is moving toward no-bleed air environmental control systems (ECS), variable-frequency (VF) power distribution systems, and electrical actuation.
Military ground vehicles have migrated toward hybrid electric technology, where the main propulsion is performed by electric drives. Therefore, substantial demand for increased power generation has emerged. Future space vehicles will require electric power generation systems for thrust vector and flight control actuation. These systems must be more robust and offer greatly reduced operating costs and safety compared to the existing Space Shuttle power systems.
These new aerospace trends have significantly increased power generation needs. This has led to increased operating voltages to reduce system losses, weight, and volume. New power, quality and electromagnetic interference (EMI) requirements have been created to satisfy both quality and performance needs. The overall result has been a significant increase in the installed electric power, creating challenges in accommodating this equipment in the new platforms. Therefore, overall system performance improvement and power density increases are necessary for the new-generation hardware to satisfy MEA. Decreasing the cost of power generation systems will make the new platforms more affordable.
Wide Speed Range (WSR) PGS applicable to MEA must satisfy a complex set of requirements. The main function of such a system is electrical power generation; hence the system must provide conversion of the mechanical power supplied by the prime mover to conditioned electrical power supplied to the distribution bus. Generation is typically defined as continuous power at 100 percent load. Increasing the load to 150 percent for a limited time may be required. The percentage of increase and time required for overloading varies from application to application.
Another requirement for WSR PGS applicable to MEA is steady-state regulation, which requires that the system maintain the output voltage constant within certain limits when the loads and other conditions are changed gradually. Transient regulation is a requirement that the system maintains the output voltage constant within certain limits when the loads and other conditions are changed rapidly. Transient limits are typically wider than steady-state limits. Typical regulation requirements can be found in MIL-STD-704E. Electromagnetic interference (EMI), both conducted and radiated emissions, are important requirements for an EPGS to provide proper operation of the installed electronics. At the same time, the electronic equipment including PGS should not be susceptible to the specified radiated emissions.
DC bus short-circuit protection is another requirement which must provide adequate protection when an external short-circuit fault occurs at the DC distribution bus. Feeder short-circuit protection function is also required to prevent excessive current flow in the electric machine and the interface electric machine power electronics to reduce damages that may lead to a hazardous condition. Power electronics short-circuit protection is required to prevent excessive current flow in the power electronics unit. Overvoltage protection is required to prevent excessive voltage across a power distribution bus. Overvoltage protection prevents damage of the electronics connected to the distribution bus.
Electric machines used in auxiliary power unit (APU) applications typically operate at constant speed or with small variation. The main engines of an airplane normally operate with a speed range where the ratio of maximum to minimum operating speed is about 2 to 1. This speed variation creates additional difficulties for a power generation system in providing regulated power within the entire speed range. There are some applications where the speed of the prime mover, for instance a helicopter engine, changes by a factor of up to 20. This wide speed range creates even more challenges due to variation of the electromotive force (emf) voltage of the machine with the speed.
The synchronous permanent magnet machine (PMM) presents a very competitive design that outperforms other electric machines in most applications when weight and size are critical. However, the rotor flux in a typical PMM is fixed and cannot be controlled or disengaged when a short-circuit is initiated. Unlike other machines where the excitation of the rotor flux can be controlled and even disabled quickly, a PMM continues to generate emf until the rotor stops rotating. Therefore, the PMM presents a hazard in some applications, leading to its limited use, particularly in the aerospace industry.
The High Reactance Permanent Magnet Machine (HRPMM) is one type of PMM in which, should it become shorted, the phase current magnitude can be internally limited to levels capable of being sustained either indefinitely, within the thermal limits of the system, or until the rotor speed can be reduced to zero. In some prior HRPMM power topologies the functional and protection requirements may be resolved. However, the operating speed range may still be quite narrow.
As can be seen, there is a need for a PMM-based power generation systems that can supply power to a DC bus within a wide speed variation while satisfying the functional and safety requirements discussed above.
In one aspect of the invention, a device for controlling a variable speed electrical power generator comprises: a permanent magnet machine generating an output voltage across output terminals, the permanent magnet machine having a plurality of stator windings; a diode bridge connected across the plurality of stator windings; a transistor for at least temporarily short-circuiting the diode bridge; a capacitor for smoothing the output voltage detected across the pair of output terminals; and a control unit for generating a signal that switches the transistor in response to a voltage detected across the pair of output terminals, the control unit signal modifying the duty cycle of the switching of the transistor in response to variations in the speed of the power generator to maintain a desired voltage across the pair of output terminals.
In another aspect of the invention a variable speed permanent magnet machine connected to a load comprises: a permanent magnet rotor; a stator assembly mounted adjacent the rotor and including a plurality of electrical windings disposed in a plurality of slots between a plurality of stator teeth and having a stator winding resistance RS, the electrical windings being electrically connected to a permanent magnet machine output adapted to deliver generated output voltage from the permanent magnet machine; a voltage control circuit providing for a boost in the output voltage in a first rotational speed range, the voltage control circuit also providing limiting of output current to a pre-selected value in a second rotational speed range; wherein, in use, the movement of the rotor induces an alternating voltage and current in the electrical windings of a first polarity and the first alternating voltage and current induces a second alternating voltage and current of a second polarity in the electrical windings, and the voltage control circuit limiting of output current being provided by the second alternating voltage and current of a second polarity.
In a further aspect of the present invention, a method for controlling a wide speed range high reactance permanent magnet machine in a plurality of speed ranges comprises: determining an output voltage across output terminals of a circuit including a wide speed range high reactance permanent magnet machine having stator windings, a diode bridge connected across the stator windings, a solid state switch connected across the diode bridge and a PWM controller circuit connected to the solid state switch; if the wide speed range high reactance permanent magnet machine is in a low speed range, and if the detected output voltage is lower than a desired output voltage, increasing the duty cycle of the PWM controller to increase the detected output voltage; and if the detected output voltage is higher than the desired voltage, decreasing the duty cycle of said PWM controller to decrease the detected output voltage.
These and other features, aspects and advantages of the present invention will become better understood with reference to the following drawings, description and claims.
The following detailed description is of the best currently contemplated modes of carrying out the invention. The description is not to be taken in a limiting sense, but is made merely for the purpose of illustrating the general principles of the invention, since the scope of the invention is best defined by the appended claims.
The present invention generally provides a wide speed range, high reactance permanent magnet machine (HRPMM) that may provide regulated voltage over wide variations in the rotational speed of the prime mover, and hence the HRPMM rotor. For example, the ratio of the maximum to minimum rotor speed may be as high as 20 to 1. At low machine rotational speeds, in a boost mode, the output voltage may be increased by using a pulse width modulated switch across a diode bridge to store energy in the electric machine and transfer this energy to the electric machine output. As the machine speed increases, the duty cycle of the switch may be increased to increase the output voltage. At high machine speeds, in a current limiting mode, the synchronous reactance of the HRPMM may be used to limit the current to the desired level, while the pulse width modulated switch may maintain a relatively constant duty cycle. This may be done by designing the machine parameters such that the short-circuit current is close to the operating current.
The present invention may be applicable to high speed generators where the voltage to a DC power distribution bus must be regulated over a wide speed range. One example is in helicopters where the speed of the prime mover of the generator may vary by a factor of 20 to 1. The present invention also provides an optimized solution for power generation in various applications such as MEA systems in aircraft and spacecraft, hybrid electric ground vehicles and other applications where weight and size are critical, including auxiliary power units.
Prior art based PGSs have not generally been able to provide a regulated voltage over wide rotor speed ranges. In contrast, the present invention can provide regulated voltage over rotor speed ranges as wide as 20 to 1. Further, unlike the prior art, the present invention employs a varying duty cycle of a pulse width modulated switch at slow machine speeds and close to constant duty cycle at high machine speeds. Prior art permanent magnet machines also have generally used separate inductors to provide voltage boost. In contrast, the present invention may use the inductance of the PMM to provide a voltage boost instead of using a separate inductor for this purpose.
Also shown in
A conventional aluminum housing 30 may surround the stator 12. An aluminum spacer 32 with air cooling slots 34 may be provided between the housing 30 and the spacer 32 to provide additional means for cooling the HRPMM 10.
The short-circuit current point 120 may be approximately the same for all V-I curves. This phenomenon may be due to the relation expressed in equation 2, as shown below, where RS can be ignored with a good approximation for practical purposes. While not explicitly shown in
In accordance with one embodiment of the invention, the HRPMM 10 may be designed with particular dimensions and materials to meet certain requirements. As a high reactance PMM it should have a synchronous reactance in the range of 1 m to 10 m. Also, as described below, the HRPMM may be configured such that the operating current across terminals 69, 71 is equal to the short-circuit current, that is, the current across terminals 69, 71 when load 64 is shorted, as described below.
In accordance with the invention, an HRPMM 10 that meets the above-discussed objectives is configured with various PMM parameters determined as described below. Key parameters of a HRPMM may be the phase-generated voltage EEMF, and the synchronous impedance of the machine ZS. If these two values are known explicitly, the mathematical analysis of the HRPMM may be relatively straightforward. The generated current, IM, can be calculated, utilizing circuit analysis theory, as follows:
In Equation (1), RS is the stator winding resistance and XS is the synchronous reactance. The load 64 is represented by RL (load resistance), XL (reactance) and XC (load admittance). The load resistance absorbs the real power delivered by the generator. The reactance represents the reactive load with inductive nature and the admittance represents the reactive load with capacitive behavior.
The short-circuit current of the HRPMM 10, for example the current at terminals 38, 40, and 42 when the load 64 is shorted, can be obtained from Equation (1) by postulating the load parameters to equal zero. The result is Equation (2).
The short-circuit current depends primarily on two basic machine parameters, EEMF and ZS. For a conventional PMM, EEMF and ZS may be selected such that the short-circuit current is several times larger than the operating or nominal current. A reactance-per-unit quantity can be introduced to define the relative reactance (reactance per unit) XPU=IRATED/ISC. For a conventional reactance machine, XPU may be from 0.2 to 0.3. In contrast, for the HRPMM 10 in accordance with one embodiment of the invention, EEMF and ZS are selected in such a way that the short-circuit current between terminals 69, 71 is similar to the operating current and XPU is from 0.8 to 1.0. One skilled in the art will appreciate the particular physical and electrical features of the HRPMM 10 that may be configured using known design techniques to achieve this XPU.
There are two distinct regions in the regulation curve 122: a boost region 124 and a current limiting region 126. The boost region 124 occurs when the rectified machine voltage across input terminals 57 and 59 is below the output regulated voltage across terminals 69, 71. In the boost region 124, approximately in the range of 80 Hz to 180 Hz, the solid state switch 58 may short the machine terminals 57, 59 in order to increase the current across terminals 57 and 59 and store more energy in the machine winding 14. Upon the opening of solid state switch 58, the energy may be released from the winding 14 to the capacitor 62. In this way, a voltage boosting operation, which increases the output voltage across terminals 69, 71, may be achieved. Boosting operation is described in equation 3 where Vout is the output regulated voltage across terminals 69, 71, VL-L P is the input boosted voltage across terminals 57, 59, which is in fact the machine line-to-line peak voltage, and D is the duty cycle. The duty cycle is defined as D=ton/T where T is the period of the PWM signal on line 72 for solid state switch 58 and ton is the on-time of the PWM signal. Equation 3 does not account for the non-ideal characteristics of the diodes, switches and electric machine.
When the HRPMM 10 operates at the lowest speed, the frequency may be 80 Hz and the back emf voltage may be 7.55 Vrms L-N, as shown in curve 118 in
As the speed of the HRPMM 10 is increased in the boost region 124, the frequency and back emf voltage increase and lower duty cycle may be required. Another data point 128 shown in
Above about 210 Hz, for example, at data point 134, the voltage control circuit 36 may transition from the boosting mode 124 to the current limiting mode 126. The duty cycle of the regulation curve may remain relatively constant for the high frequencies of the current limiting region 126. Thus, in the lower speed region 124, a higher duty cycle may boost the output voltage, but in the high speed region, from about 180 Hz to about 210 Hz, increases in the duty cycle will lower the output voltage. Above 210 Hz the duty cycle has a small effect on output voltage, because of current limiting as discussed below. A characteristic point 136 may be at the highest speed of operation where the frequency may be 1,250 Hz, the back emf voltage may be 118 Vrms L-N, and the PWM may operate at 79.38 percent duty cycle. Different duty cycles values can be expected at different load values and during transients. These transients can be expected when fast speed or load changes occur.
In the current limiting mode of operation, the voltage control circuit 36 may use the synchronous reactance of the HRPMM to limit the output current. In particular, the elements of the WSR HRPMM 10 shown in
A simulation of the WSR HRPMM based EPGS shown in
Step 92 may determine if the speed of the WSR HRPMM is in the low range. This low range may correspond to the frequency range in
If step 94 determines that the detected output voltage is higher than the desired output voltage, step 96 will decrease the PWM duty cycle to lower output voltage. The process 84 may next return to step 88.
Returning now to step 92, if is determined that the WSR HRPMM is not in the low speed range, then the process may move from step 92 to step 100 which may determine if the detected output voltage is lower than the desired output voltage. If it is, the process moves to step 102 where the duty cycle is decreased to increase the output voltage. If step 100 determined that the measured output voltage was not lower than the desired output voltage, then step 104 will increase the duty cycle to decrease the output voltage, after which the process 84 may return to step 88.
As can be appreciated by those skilled in the art, the present invention provides an WSR HRPMM 10 that can deliver regulated voltage to a DC power distribution bus with a number of advantages. It can operate over an extended speed range of up to a factor of 20. It provides a simple power topology, using only one switch and seven diodes. In boost operation at low speed no dedicated inductance is required because the inductance of the electric machine is used as an energy storage element. In current limiting operation at high speed the synchronous reactance of the HRPMM is used for current limiting.
It should be understood, of course, that the foregoing relates to exemplary embodiments of the invention and that modifications may be made without departing from the spirit and scope of the invention as set forth in the following claims.
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|U.S. Classification||322/46, 322/44, 322/47, 322/54|
|Cooperative Classification||H02P9/10, H02P2101/30|
|May 21, 2007||AS||Assignment|
Owner name: HONEYWELL INTERNATIONAL INC., NEW JERSEY
Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:GANEV, EVGENI;DRUZSBA, ANDREW R.;ALKHATIB, ADDY FOUAD;REEL/FRAME:019322/0929
Effective date: 20070518
|Feb 25, 2013||FPAY||Fee payment|
Year of fee payment: 4